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- Wind-tunnel investigation of perforated split flaps for use as dive brakes on a rectangular NACA 23012 airfoil
- Aerodynamic characteristics and flap loads of perforated double split flaps on a rectangular NACA 23012 airfoil
- Aerodynamic Characteristics of Several Modifications of a 0.45-Scale Model of the Vertical Tail of the Curtiss XP-62 Airplane
- Preliminary Investigation of Various Ailerons on a 42 Degree Sweptback Wing for Lateral Control at Transonic Speeds
- Aerodynamic characteristics at subsonic and transonic speeds of a 42.7 degree sweptback wing model having an aileron with finite trailing-edge thickness
- Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds
- Maximum-Lift Investigation of a 1/40-Scale X-1 Airplane Wing at Mach Numbers From 0.60 to 1.15
- Maximum-Lift Investigation at Mach Numbers From 0.05 to 1.20 of a Wing With Leading Edge Swept Back 42 Degrees
- Effects of rate of flap deflection on flap hinge moment and wing lift through the Mach number range from 0.32 to 0.87
- Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds
- Wind-Tunnel Investigation at Transonic Speeds of a Jet Control on an 80 Degree Delta-Wing Missile
- A wind-tunnel investigation of the development of lift on wings in accelerated longitudinal motion